CN209381573U - A kind of composite aircraft relief printing plate - Google Patents
A kind of composite aircraft relief printing plate Download PDFInfo
- Publication number
- CN209381573U CN209381573U CN201822068160.6U CN201822068160U CN209381573U CN 209381573 U CN209381573 U CN 209381573U CN 201822068160 U CN201822068160 U CN 201822068160U CN 209381573 U CN209381573 U CN 209381573U
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- CN
- China
- Prior art keywords
- plate
- relief printing
- printing plate
- screw rod
- intaglio
- Prior art date
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Abstract
The utility model discloses a kind of composite aircraft relief printing plates, including intaglio plate, guide plate and relief printing plate, docking groove is offered in the plate face of intaglio plate, official documents and correspondence slot is offered on the bottom surface of docking groove, and continuous hopper is offered on the side wall of docking groove, continuous hopper is internally provided with postive stop baffle, rotation slot is provided in the plate face of postive stop baffle, the inner rotation of rotation slot is connected with adjusting screw rod, adjusting screw rod is screwed on the bottom surface of operating groove, operating groove is provided with the upper surface of intaglio plate, extension plate is welded on the outer wall of intaglio plate, the upper surface of extension plate is welded with guide plate, guide plate is plugged on the inside of retaining ring;The utility model proposes composite aircraft relief printing plate pass through with concave-convex two pieces of printing plates, needs, the convex image carving of machine makes one piece of intaglio plate, one piece of relief printing plate respectively on two pieces of embossing plates on the printer, various patterns can be extruded on printed material, indent and convex feel is touched up with hand, enhances the three-dimensional sense of printed matter.
Description
Technical field
The utility model relates to gilding press protrusive board correlative technology field, specially a kind of composite aircraft relief printing plate.
Background technique
It is gold stamping, also make thermoprint, is a kind of printing decoration technique, is to heat metallic plate, applies foil, imprinted on printed matter
Golden text or pattern out, gold stamping to have clear patterns, beauty with the rapid development of stamping systems and packaging industry, color is fresh
Gorgeous brilliant, wear-resisting, weather-proof feature, gilding press are exactly the equipment for completing gilding technology;
In the prior art, gilding press carries out thermoprint to material using machine protrusive board, although may be implemented aluminium film thermoprint in material
On material, but the pattern of its thermoprint is plane drawing, is touched up with hand and does not have indent and convex feel, printed matter is made to lack three-dimensional sense;For
This, the utility model proposes a kind of composite aircraft relief printing plates for solving the above problems.
Summary of the invention
The purpose of this utility model is to provide a kind of composite aircraft relief printing plates, to solve mentioned above in the background art ask
Topic.
To achieve the above object, the utility model provides the following technical solutions: a kind of composite aircraft relief printing plate, including intaglio plate, leads
To plate and relief printing plate, docking groove is offered in the plate face of the intaglio plate, official documents and correspondence slot is offered on the bottom surface of the docking groove, and right
Offer continuous hopper on the side wall of access slot, the continuous hopper is internally provided with postive stop baffle, in the plate face of the postive stop baffle
It is provided with rotation slot, the inner rotation of the rotation slot is connected with adjusting screw rod, and the adjusting screw rod is screwed onto the bottom of operating groove
On face, the operating groove is provided with the upper surface of intaglio plate, and extension plate, the upper surface of the extension plate are welded on the outer wall of intaglio plate
It is welded with guide plate, the guide plate is plugged on the inside of retaining ring, and the retaining ring is welded on the side wall of relief printing plate, at the relief printing plate
In the top of intaglio plate, and integrally formed with official documents and correspondence plate on the bottom surface of relief printing plate, the official documents and correspondence plate is docked at the inside of official documents and correspondence slot.
Preferably, the continuous hopper is in rectangular cylinder structure, is continued there are two hopper settings, two continuous hoppers are about docking groove
Central symmetry distribution, the height for continuing hopper is less than the height of docking groove, and docking groove is coplanar with the bottom surface of continuous hopper.
Preferably, the postive stop baffle is in rectangular plate-like structure, and the width of postive stop baffle is less than the width of continuous hopper, rotation
Slot is in T-shaped circular cylinder structure, and the rotation lesser notch of groove area is in the upper surface of postive stop baffle, and rotation slot is to adjusting
Screw rod is limited, and the part that adjusting screw rod is in inside rotation slot is not provided with screw thread, adjusting screw rod circular columns in the shape of an " I "
Body structure.
Preferably, the L-shaped plate structure of the guide plate, insertion is equipped with multiple steel in the vertical plate face of guide plate
Pearl, the bending level board of guide plate are in the top of retaining ring always.
Preferably, the retaining ring is in " Fang " shape rectangular plate-like structure, and two end faces of retaining ring are welded on the side of relief printing plate
On wall, there are two the settings of official documents and correspondence plate, and two official documents and correspondence plates are distributed about the central symmetry of relief printing plate.
Compared with prior art, the utility model has the beneficial effects that
1. the utility model proposes composite aircraft relief printing plate pass through with concave-convex two pieces of printing plates, need on the printer machine it is convex
Image carving makes one piece of intaglio plate, one piece of relief printing plate respectively on two pieces of embossing plates, can extrude on printed material various
Pattern touches up indent and convex feel with hand, enhances the three-dimensional sense of printed matter;
2. the utility model proposes composite aircraft relief printing plate postive stop baffle is set in continuous hopper, postive stop baffle is in adjusting screw rod
Drive under move up and down, material is limited, it is avoided significantly to jolt up and down;
3. the utility model proposes composite aircraft relief printing plate guide frame is added between intaglio plate and relief printing plate, avoid two versions right
Occur misplacing and leading to thermoprint deviation when connecing.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model;
Fig. 2 is structure enlargement diagram at A in Fig. 1.
In figure: intaglio plate 1, docking groove 2, official documents and correspondence slot 3, continuous hopper 4, postive stop baffle 5, rotation slot 6, adjusting screw rod 7, operating groove
8, extension plate 9, guide plate 10, retaining ring 11, relief printing plate 12, official documents and correspondence plate 13.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1 to Fig. 2 is please referred to, the utility model provides a kind of technical solution: a kind of composite aircraft relief printing plate, including intaglio plate 1, lead
To plate 10 and relief printing plate 12, docking groove 2 is offered in the plate face of intaglio plate 1, official documents and correspondence slot 3 is offered on the bottom surface of docking groove 2, and right
Continuous hopper 4 is offered on the side wall of access slot 2, continuous hopper 4 is internally provided with postive stop baffle 5, is arranged in the plate face of postive stop baffle 5
There is rotation slot 6, the inner rotation of rotation slot 6 is connected with adjusting screw rod 7, and adjusting screw rod 7 is screwed on the bottom surface of operating groove 8, behaviour
Make the upper surface that slot 8 is provided with intaglio plate 1, extension plate 9 is welded on the outer wall of intaglio plate 1, the upper surface of extension plate 9 is welded with guiding
Plate 10, guide plate 10 are plugged on the inside of retaining ring 11, and retaining ring 11 is welded on the side wall of relief printing plate 12, and relief printing plate 12 is in intaglio plate 1
Top, and integrally formed with official documents and correspondence plate 13 on the bottom surface of relief printing plate 12, official documents and correspondence plate 13 is docked at the inside of official documents and correspondence slot 3.
Further, continuing hopper 4 is in rectangular cylinder structure, is continued there are two the settings of hopper 4, two continuous hoppers 4 are about docking
The central symmetry of slot 2 is distributed, and the height for continuing hopper 4 is less than the height of docking groove 2, and docking groove 2 is coplanar with the bottom surface of continuous hopper 4,
Material is injected in continuous hopper 4, adjusting screw rod 7 is then screwed at operating groove 8, postive stop baffle 5 is driven to move in continuous hopper 4,
Postive stop baffle 5 is pushed into the top of material or is taken out with material convenient for material without making adjusting screw rod 7 to paper material clamping
Out.
Further, postive stop baffle 5 is in rectangular plate-like structure, and the width of postive stop baffle 5 is less than the width of continuous hopper 4, turns
Dynamic slot 6 is in T-shaped circular cylinder structure, and the lesser notch of 6 area of rotation slot is in the upper surface of postive stop baffle 5, rotation slot 6
Adjusting screw rod 7 is limited, the part that adjusting screw rod 7 is in inside rotation slot 6 is not provided with screw thread, and adjusting screw rod 7 is in " work "
Font circular cylinder structure, adjusting screw rod 7 are screwed on the bottom surface of operating groove 8, and the bottom end of adjusting screw rod 7 is rotatably connected on
Therefore the inside of dynamic slot 6 when adjusting screw rod 7 rotates, drives postive stop baffle 5 to move inside continuous hopper 4.
Further, the L-shaped plate structure of guide plate 10, insertion is equipped with multiple steel in the vertical plate face of guide plate 10
Pearl, the bending level board of guide plate 10 is in the top of retaining ring 11 always, during relief printing plate 12 moves down, retaining ring 11 along
Guide plate 10 slides, and avoids docking between relief printing plate 12 and intaglio plate 1 from deviation occur, and the steel ball of 10 plate face of guide plate reduces guide plate
Abrasion between 10 and retaining ring 11.
Further, retaining ring 11 is in " Fang " shape rectangular plate-like structure, and two end faces of retaining ring 11 are welded on relief printing plate 12
Side wall on, official documents and correspondence plate 13 setting there are two, two official documents and correspondence plates 13 about relief printing plate 12 central symmetry be distributed.
Working principle: in actual work, material is injected in continuous hopper 4, adjusting screw rod 7 is then screwed at operating groove 8
Drive postive stop baffle 5 moved in continuous hopper 4, by postive stop baffle 5 be pushed into material top or and material, adjusted without making
Screw rod 7 is saved to paper material clamping, is extracted out convenient for material, relief printing plate 12 moves down the inside for being docked at docking groove 2, and official documents and correspondence plate 13 pushes
Material in continuous hopper 4, and docking with official documents and correspondence slot 3, so that relief pattern at the surface thermoprint of material, relief printing plate 12 is to moving down
In dynamic process, retaining ring 11 is slided along guide plate 10, and docking between relief printing plate 12 and intaglio plate 1 is avoided deviation, and guide plate occur
The steel ball of 10 plate faces reduces the abrasion between guide plate 10 and retaining ring 11.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of composite aircraft relief printing plate, including intaglio plate (1), guide plate (10) and relief printing plate (12), it is characterised in that: the intaglio plate
(1) it offers in plate face docking groove (2), is offered official documents and correspondence slot (3) on the bottom surface of the docking groove (2), and docking groove (2)
It is offered on side wall continuous hopper (4), the continuous hopper (4) is internally provided with postive stop baffle (5), the postive stop baffle (5)
It is provided in plate face rotation slot (6), the inner rotation of the rotation slot (6) is connected with adjusting screw rod (7), the adjusting screw rod
(7) it is screwed on the bottom surface of operating groove (8), the operating groove (8) is provided with the upper surface of intaglio plate (1), on the outer wall of intaglio plate (1)
It is welded with extension plate (9), the upper surface of the extension plate (9) is welded with guide plate (10), and the guide plate (10) is plugged on button
The inside of ring (11), the retaining ring (11) are welded on the side wall of relief printing plate (12), and the relief printing plate (12) is in the upper of intaglio plate (1)
Portion, and integrally formed with official documents and correspondence plate (13) on the bottom surface of relief printing plate (12), the official documents and correspondence plate (13) is docked at the interior of official documents and correspondence slot (3)
Portion.
2. a kind of composite aircraft relief printing plate according to claim 1, it is characterised in that: the continuous hopper (4) is in rectangular cylinder knot
Structure continues there are two hopper (4) settings, and two continuous hoppers (4) are distributed about the central symmetry of docking groove (2), continue the height of hopper (4)
Degree is less than the height of docking groove (2), and docking groove (2) is coplanar with the bottom surface of continuous hopper (4).
3. a kind of composite aircraft relief printing plate according to claim 1, it is characterised in that: the postive stop baffle (5) is in rectangular plate-like
Structure, the width of postive stop baffle (5) are less than the width of continuous hopper (4), and rotation slot (6) is in T-shaped circular cylinder structure, rotation
The lesser notch of slot (6) area is in the upper surface of postive stop baffle (5), and rotation slot (6) limits adjusting screw rod (7), adjusts
Section screw rod (7) is in the internal part of rotation slot (6) and is not provided with screw thread, adjusting screw rod (7) circular cylinder structure in the shape of an " I ".
4. a kind of composite aircraft relief printing plate according to claim 1, it is characterised in that: the L-shaped plate of the guide plate (10)
Structure, insertion is equipped with multiple steel balls in the vertical plate face of guide plate (10), and the bending level board of guide plate (10) is in always
The top of retaining ring (11).
5. a kind of composite aircraft relief printing plate according to claim 1, it is characterised in that: the retaining ring (11) is in " Fang " shape rectangle
Two end faces of plate structure, retaining ring (11) are welded on the side wall of relief printing plate (12), and there are two official documents and correspondence plate (13) settings, and two
Official documents and correspondence plate (13) is distributed about the central symmetry of relief printing plate (12).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201822068160.6U CN209381573U (en) | 2018-12-09 | 2018-12-09 | A kind of composite aircraft relief printing plate |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201822068160.6U CN209381573U (en) | 2018-12-09 | 2018-12-09 | A kind of composite aircraft relief printing plate |
Publications (1)
Publication Number | Publication Date |
---|---|
CN209381573U true CN209381573U (en) | 2019-09-13 |
Family
ID=67871378
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201822068160.6U Expired - Fee Related CN209381573U (en) | 2018-12-09 | 2018-12-09 | A kind of composite aircraft relief printing plate |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN209381573U (en) |
-
2018
- 2018-12-09 CN CN201822068160.6U patent/CN209381573U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190913 Termination date: 20201209 |
|
CF01 | Termination of patent right due to non-payment of annual fee |